Method for manufacturing anodized aluminum alloy parts without surface discoloration

Patent metadata

Field	Value
Publication number	US-10030294-B2
Application number	US-201514622998-A
Country	US
Kind code	B2
Filing date	Feb 16, 2015
Priority date	Feb 16, 2015
Publication date	Jul 24, 2018
Grant date	Jul 24, 2018

Abstract

A method for manufacturing a part including steps of providing an aluminum starting material, wherein the aluminum starting material is in an anneal temper, cold working the aluminum starting material to obtain an aluminum cold worked material, and forming the part from the aluminum cold worked material.

First claim

What is claimed is:

1. A method for manufacturing a part comprising:
providing an aluminum starting material, wherein said aluminum starting material is in an anneal temper;
cold working said aluminum starting material such that substantially uniform stresses are introduced therein to obtain an aluminum cold worked material;
forming said part from said aluminum cold worked material having said substantially uniform stresses therein such that non-uniform stresses are introduced to the aluminum cold worked material, wherein said forming includes forming said part to have a non-planar configuration;
solution heat treating said part having said substantially uniform stresses therein and having said non-inform stresses therein, thereby yielding a solution heat treated part having a recrystallized grain structure;
aging said solution heat treated part; and
anodizing said aged part.

2. The method of claim 1 wherein said part is an aircraft lipskin.

3. The method of claim 1 wherein said aluminum starting material comprises a 2xxx series aluminum alloy.

4. The method of claim 1 wherein said aluminum starting material comprises 2219 aluminum alloy.

5. The method of claim 1 wherein said aluminum starting material is in plate form.

6. The method of claim 1 wherein said cold working comprises stretching said aluminum starting material.

7. The method of claim 1 wherein said cold working comprises rolling said aluminum starting material.

8. The method of claim 1 wherein said cold working is performed at a cold working temperature, and wherein said cold working temperature is at most about 50 percent of a melting point, in degrees kelvin, of said aluminum starting material.

9. The method of claim 1 wherein said cold working is performed at a cold working temperature, and wherein said cold working temperature is at most about 300° F.

10. The method of claim 1 wherein said cold working is performed at a cold working temperature, and wherein said cold working temperature is at most about 200° F.

11. The method of claim 1 wherein said cold working is performed to achieve at least about 2 percent cold work.

12. The method of claim 1 wherein said cold working is performed to achieve about 3 percent to about 20 percent cold work.

13. The method of claim 1 wherein said cold working is performed to achieve about 5 percent to about 15 percent cold work.

14. The method of claim 1 wherein said step of providing an aluminum starting material comprises:
casting an ingot;
scalping said ingot to yield a scalped ingot;
homogenizing said scalped ingot to yield a homogenized ingot;
breakdown of said homogenized ingot to yield a slab;
rolling said slab to yield a rolled aluminum material; and
annealing said rolled aluminum material to yield said aluminum starting material.

15. The method of claim 1 wherein said forming comprises at least one of spin forming and die-stamping.

16. The method of claim 1 wherein said aluminum starting material includes a plurality of individual grains, and wherein said cold working results in accumulation of strain energy in said individual grains of said aluminum cold worked material.

17. A method for manufacturing a part comprising:
providing an aluminum starting material, wherein said aluminum starting material is an annealed and cold worked condition, said aluminum cold worked material having substantially uniform stresses therein;
forming said part from said aluminum cold worked material having said substantially uniform stresses therein such that non-uniform stresses are introduced to the aluminum cold worked material, wherein said forming includes forming said part to have a non-planar configuration;
solution heat treating said part having said substantially uniform stresses therein and having said non-uniform stresses therein, thereby yielding a solution heat treated part having a recrystallized grain structure; and
anodizing said solution heat treated part.

18. The method of claim 17 wherein said non-planar configuration is a lipskin configuration.

19. The method of claim 18 wherein said forming said part to have said lipskin configuration comprises:
cutting said aluminum cold worked material into a blank having a flat, annular ring shape; and
forming said blank into said lipskin configuration having said non-planar configuration.

20. The method of claim 1 wherein said non-planar configuration is a lipskin configuration.

Assignees

• Boeing Co

Inventors

• Gane David H
• Glamm Ryan J
• Weber Gary R
• Johnson Ricole A
• Tomt Terry C
• Pugh Azzréal
• Kane Daniel J
• Verge Peter D

Classifications

• B23P15/00

  Making specific metal objects by operations not covered by a single other subclass or a group in this subclass · CPC title

• C22F1/04 Primary

  of aluminium or alloys based thereon · CPC title

• C21D9/0081

  for slabs; for billets · CPC title

• C25D11/04

  of aluminium or alloys based thereon · CPC title

• C22C21/12

  with copper as the next major constituent · CPC title